View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 33591U 09005A 22179.54051896 .00000124 00000-0 91813-4 0 9997
2 33591 99.1467 213.9100 0014437 153.3179 206.8738 14.12581742689757
| Epoch (UTC): | 28 June 2022 12:58:20 |
| Eccentricity: | 0.0014437 |
| inclination: | 99.1467° |
| perigee height: | 840 km |
| apogee height: | 861 km |
| right ascension of ascending node: | 213.9100° |
| argument of perigee: | 153.3179° |
| revolutions per day: | 14.12581742 |
| mean anomaly at epoch: | 206.8738° |
| orbit number at epoch: | 68975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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